Rolls-Royce Conway (jet engine)
GPTKB entity
Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:military
civil aviation |
| gptkbp:bypassRatio |
0.3:1
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:diameter |
45 in (1.14 m)
|
| gptkbp:enteredService |
1950s
|
| gptkbp:firstRun |
1950
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Conway (jet engine)
|
| gptkbp:length |
146 in (3.71 m)
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce
|
| gptkbp:notableFor |
first turbofan engine to enter service
|
| gptkbp:numberOfStages |
2 (high pressure), 2 (low pressure)
9 (low pressure), 7 (high pressure) |
| gptkbp:predecessor |
gptkb:Rolls-Royce_Avon
|
| gptkbp:retired |
1980s
|
| gptkbp:successor |
gptkb:Rolls-Royce_RB211
|
| gptkbp:thrust |
17,500 lbf (77.8 kN)
|
| gptkbp:type |
turbofan
|
| gptkbp:usedInAircraft |
gptkb:Vickers_VC10
gptkb:aircraft gptkb:Douglas_DC-8 gptkb:Handley_Page_Victor |
| gptkbp:weight |
4,850 lb (2,200 kg)
|
| gptkbp:bfsParent |
gptkb:Conway
|
| gptkbp:bfsLayer |
6
|